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A Pareto front based on mass and cross range objective functions was generated, highlighting the existence of several design scenarios: minimum mass, maximum winglet, maximum cross range.
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It is recognized that the winglet location suitable for maximum augmentation can be defined in two ways, one that delivers maximum enhancement while ignoring the increase in flow loss and the other that incurs justifiable increase in the flow loss.
The maximum cruising speed is 6km for all Winglet versions.
In order to find the best winglet shape among the winglets on the Pareto front, three figures of merit are used: the aircraft Maximum Takeoff Weight (MTOW), the aircraft fuel weight and the aircraft Direct Operating Cost (DOC).
"Maximum freedom".
Maximum value?
Maximum learning.
Maximum violence.
Maximum Electronic Rock n Roll".
She got the maximum.
Minimal input, maximum output.
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